Numerical simulation of shock-induced combustion generated by high-speed projectiles in detonable gas mixtures
Author:
Affiliation:
1. Washington, University, Seattle
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1989-673
Reference32 articles.
1. Morphology of a standing oblique detonation wave
2. Ram accelerator - A new chemical method for accelerating projectilesto ultrahigh velocities
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